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GB1571611A - Internal combustion engines - Google Patents

Internal combustion engines Download PDF

Info

Publication number
GB1571611A
GB1571611A GB27910/76A GB2791076A GB1571611A GB 1571611 A GB1571611 A GB 1571611A GB 27910/76 A GB27910/76 A GB 27910/76A GB 2791076 A GB2791076 A GB 2791076A GB 1571611 A GB1571611 A GB 1571611A
Authority
GB
United Kingdom
Prior art keywords
cylinder
piston
air
internal combustion
dead centre
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB27910/76A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Outboard Marine Corp
Original Assignee
Outboard Marine Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Outboard Marine Corp filed Critical Outboard Marine Corp
Priority to GB27910/76A priority Critical patent/GB1571611A/en
Priority to US05/808,075 priority patent/US4162663A/en
Priority to CA281,900A priority patent/CA1072450A/en
Priority to JP8035877A priority patent/JPS5311211A/en
Priority to SE7707818A priority patent/SE432126B/en
Publication of GB1571611A publication Critical patent/GB1571611A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B17/00Engines characterised by means for effecting stratification of charge in cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/12Other methods of operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/18DOHC [Double overhead camshaft]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

PATENT SPECIFICATION ( 11) 1571611
( 21) Application No 27910/76 ( 22) Filed 5 July 1976 ( 19) ( 23) Complete Specification filed 5 July 1977 ( 44) Complete Specification published 16 July 1980 ( 51) INT CL 3 F 02 B 25/06 ( 52) Index at acceptance FIB IB 9 1 Gl K 1 GX 15 2 A 11 B 2 A 18 2 A 9 A ( 72) Inventor JOSEPH EHRLICH ( 54) IMPROVEMENTS IN OR RELATING TO INTERNAL COMBUSTION ENGINES ( 71) We, OUTBOARD MARINE CORPORATION, a Body Corporate organised under the laws of the State of Delaware, United States of America, of 100 Seahorse Drive, Waukegan, Illinois 60085, United States of America, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and
by the following statement: -
This invention relates to internal combustion engines and more particularly to four stroke internal combustion engines, and offers improvements in introducing air to the cylinder of an internal combustion engine during a suction or induction stroke.
According to the invention, an internal combustion engine comprises a cylinder, a piston movable in said cylinder between top dead centre and bottom dead centre positions, an air entry port located in said cylinder immediately above said piston when said piston is at bottom dead centre and adapted to be opened and closed by the piston in response to piston movement, and a reed valve associated with said air entry port for preventing flow through the port from the cylinder and permitting flow through the port to the cylinder.
In a four stroke engine, the arrangement is preferably such that the piston moves to bottom dead centre from a head end of the cylinder, which head end is associated with a main inlet port adapted to be closed as said piston in a suction stroke approaches bottom dead centre It is also possible to have an engine driven pump for presurising the air for entry into the cylinder through an air entry port or ports.
In a preferred form of the invention, the or each air entry port opened by the piston at bottom dead centre is directed generally tangentially of the cylinder, i e is directed to lead inlet air round the cylinder against the inside wall thereof Hence in operation of the engine, air through the said port or ports enters the cylinder with a swirling movement mainly between the indrawn charge and the cylinder wall whereby stratification and turbulence is achieved Conveniently there is an array of air entry ports disposed circumferentially around the cylinder wall and they may open from a local gallery surrounding the cylinder wall and communicating with atmosphere or the outlet of an engine driven pump.
The air entry port or ports are conveniently simply uncovered by the piston on the last part of the induction stroke so that the final piston movement draws the air into the cylinder Alternatively the air can enter under pressure established by a pump, or any other means.
An embodiment of the invention will now be described by way of example and with reference to the acompanying drawings, in which: Figure 1 is a sectional elevation of an engine embodying the invention, and Figure 2 is a sectional view taken along lines 2-2 in Figure 1.
Figure 1 shows how when the piston 11 is approaching bottom dead centre (it is shown in Figure 1 at bottom dead centre) the last movement of the piston on the induction stroke draws air into the cylinder 12 through air entry ports 13 arranged circumferentially around the cylinder wall Figure 2 shows that there are three ports 13 arranged circumferentially around the cylinder wall, and communicating with a surrounding chamber or gallery 14 connected to a source of air at 15 which may merely be the surrounding air or may be the outlet from a means for providing a pressurised flow of air such as a pump driven by the engine Each port 13 is fitted with a reed valve 16 permitting air to enter the cylinder when there is a pressure differential across it but preventing gas from escaping from the cylinder.
The main fuel-air inlet valve 17 is arranged to be closed by its cam 18 as the ports 13 begin to be uncovered.
On the induction stroke the piston draws in fuel/air mixture through the valve 17 which is closed as the piston approaches M F:.
1,571,611 bottom dead centre and starts to uncover the air ports 13 Thus the final movement of the piston draws air in through the ports 13 and their reed valves.
The tangential direction of the ports 13 shown in Figure 2 causes the incoming air to swirl generally as indicated at 19 which produces stratification and turbulence.
On the compression stroke the reed valves prevent escape of charge before the ports 13 are covered, and on the subsequent working stroke even after the ports are uncovered as the piston aproaches bottom dead centre the reed valves 16 will prevent loss of the ignited charge and loss of pressure.
On the exhaust stroke the burnt products of combustion are discharged through the exhaust valve 19 which is suitably opened by its cam 20.

Claims (8)

WHAT WE CLAIM IS:-
1 An internal combustion engine comprising a cylinder, a piston movable in said cylinder between top dead centre and bottom dead centre positions, an air entry port located in said cylinder immediately above said piston when said piston is at bottom dead centre and adapted to be opened and closed by the piston in response to piston movement, and a reed valve associated with said air entry port for preventing flow through the port from the cylinder and permitting flow through the port to the cylinder.
2 An internal combustion engine in accordance with claim 1, wherein said air entry port extends generally tangentially of said cylinder so that air entering said cylinder through said port swirls within said cylinder.
3 An internal combustion engine in accordance with claim 1 or 2 further including an air chamber extending at least partially circumferentially around said cylinder and communicating with a source of air, and a plurality of said air entry ports each with an associated reed valve, said ports being arranged around said cylinder in an angularly spaced series and communicating between said cylinder and said air chamber.
4 An internal combustion engine comprising a cylinder, a piston movable in said cylinder between top dead centre and bottom dead centre positions, a plurality of air entry ports located in said cylinder immediately above said piston when said piston is at bottom dead centre and adapted to be opened and closed by the piston in response to piston movement, said air entry ports being arranged around said cylinder in an angularly spaced series and extending generally tangentially of said cylinder so that air entering said cylinder through said ports swirls within said cylinder, an air chamber extending at least partially circumferentially around said cylinder and communicating with a source of air and with said plurality of air entry ports, and a separate reed valve operatively associated with each of said ports preventing flow from said cylinder to said air chamber and permitting flow into said cylinder from said chamber.
An internal combustion engine in accordance with claim 3 or 4, wherein said source of air comprises means for providing a pressurised flow of air.
6 An internal combustion engine in accordance with any one of the preceding claims, wherein said engine is a four stroke engine.
7 An internal combustion engine in accordance with claim 6, the arrangement being such that said piston moves to bottom dead centre from a head end of the cylinder, which head end is associated with a main inlet port adapted to be closed as said piston in a suction stroke approaches bottom dead centre.
8 An internal combustion engine substantially as hereinbefore described with reference to the accompanying drawings.
ARTHUR R DAVIES, Chartered Patent Agents, 27 Imperial Square, Cheltenham, and High Holborn, London, W C 1.
Agents for the Aplicants.
Printed for Her Majesty's Stationery Office by Burgess & Son (Abingdon), Ltd -1980.
Published at The Patent Office, 25 Southampton Buildings, London, WC 2 A l AY, from which copies may be obtained.
w 11 1 '1 ? J 1
GB27910/76A 1976-07-05 1976-07-05 Internal combustion engines Expired GB1571611A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB27910/76A GB1571611A (en) 1976-07-05 1976-07-05 Internal combustion engines
US05/808,075 US4162663A (en) 1976-07-05 1977-06-20 Stratified charge four-stroke engine
CA281,900A CA1072450A (en) 1976-07-05 1977-07-04 Stratified charge four-stroke engine
JP8035877A JPS5311211A (en) 1976-07-05 1977-07-05 Internal combustion engine
SE7707818A SE432126B (en) 1976-07-05 1977-07-05 INCORPORATION ENGINE, SPECIFICATION OF SPEED TYPE, WITH EFFECTIVE LAYING AND TURBULENCE IN CYLINDERS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27910/76A GB1571611A (en) 1976-07-05 1976-07-05 Internal combustion engines

Publications (1)

Publication Number Publication Date
GB1571611A true GB1571611A (en) 1980-07-16

Family

ID=10267277

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27910/76A Expired GB1571611A (en) 1976-07-05 1976-07-05 Internal combustion engines

Country Status (5)

Country Link
US (1) US4162663A (en)
JP (1) JPS5311211A (en)
CA (1) CA1072450A (en)
GB (1) GB1571611A (en)
SE (1) SE432126B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2231658C2 (en) * 2000-05-13 2004-06-27 Константин Евгеньевич Стародетко Method of operation and design of two-stroke internal combustion engine
RU2231676C1 (en) * 2003-02-14 2004-06-27 Общевойсковая Академия Вооруженных Сил Российской Федерации Heater for power plant of armored object

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4426967A (en) 1980-06-18 1984-01-24 Mcwhorter Edward M Engine charge air temperature classifier
US4649872A (en) * 1981-07-20 1987-03-17 Solheim Russell G Stratified combustion engine
IT1154300B (en) * 1982-02-23 1987-01-21 Enrico Luigi Ferraro IGNITION IGNITION ENGINE WITH VARIABLE COMPRESSION RATIO AND LOW EMISSION OF POLLUTANT GASES
JPS6263135A (en) * 1985-09-13 1987-03-19 Nippon Clean Engine Res Four-cycle internal combustion engine
FR2690951B1 (en) * 1992-05-05 1995-08-04 Melchior Jean SUPPLY METHOD FOR AN INTERNAL COMBUSTION ENGINE WITH COMPRESSION IGNITION.
RU2243386C2 (en) * 2002-02-18 2004-12-27 Чоповский Борис Петрович Internal combustion engine (versions)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1580420A (en) * 1921-09-21 1926-04-13 Dempsey Cycle Company Inc Internal-combustion engine
US1825817A (en) * 1926-11-15 1931-10-06 Walker Brooks Stratifying arrangement for internal combustion engines
US1890813A (en) * 1929-03-04 1932-12-13 Heinzelmann Hans Four-stroke internal combustion engine
US1926499A (en) * 1930-06-25 1933-09-12 Ricardo Harry Ralph Internal combustion engine of the liquid fuel injection compression ignition type
US2008089A (en) * 1931-06-27 1935-07-16 Continental Motors Corp Engine
GB406173A (en) 1932-06-24 1934-02-22 Sulzer Ag Improvements in or relating to four-stroke internal combustion engines with supercharging

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2231658C2 (en) * 2000-05-13 2004-06-27 Константин Евгеньевич Стародетко Method of operation and design of two-stroke internal combustion engine
RU2231676C1 (en) * 2003-02-14 2004-06-27 Общевойсковая Академия Вооруженных Сил Российской Федерации Heater for power plant of armored object

Also Published As

Publication number Publication date
SE7707818L (en) 1978-01-06
SE432126B (en) 1984-03-19
JPS5311211A (en) 1978-02-01
US4162663A (en) 1979-07-31
CA1072450A (en) 1980-02-26

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940705